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TUT: mesh: clean up tutorials
This commit is contained in:
Kutalmis Bercin
committed by
Andrew Heather
Andrew Heather
parent
6120e13d29
commit
3a858ac682
@ -3,12 +3,8 @@ cd "${0%/*}" || exit # Run from this directory
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. ${WM_PROJECT_DIR:?}/bin/tools/CleanFunctions # Tutorial clean functions
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#------------------------------------------------------------------------------
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cleanCase
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cleanCase0
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# Remove surface and features
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rm -rf constant/extendedFeatureEdgeMesh
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rm -f constant/triSurface/*.eMesh
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rm -f 0/pointLevel
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rm -f 0/cellLevel
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rm -rf constant
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#------------------------------------------------------------------------------
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@ -3,9 +3,16 @@ cd "${0%/*}" || exit # Run from this directory
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. ${WM_PROJECT_DIR:?}/bin/tools/RunFunctions # Tutorial run functions
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#------------------------------------------------------------------------------
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# Meshing
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mkdir -p constant
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cp -rf \
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"$FOAM_TUTORIALS"/resources/geometry/faceZoneRegions \
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constant/triSurface
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runApplication blockMesh
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runApplication surfaceFeatureExtract
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runApplication snappyHexMesh
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#------------------------------------------------------------------------------
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File diff suppressed because it is too large
Load Diff
File diff suppressed because it is too large
Load Diff
File diff suppressed because it is too large
Load Diff
@ -65,4 +65,5 @@ mergePatchPairs
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(
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);
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// ************************************************************************* //
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@ -44,4 +44,5 @@ timePrecision 6;
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runTimeModifiable true;
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// ************************************************************************* //
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@ -1,102 +0,0 @@
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: v2012 |
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| \\ / A nd | Website: www.openfoam.com |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class dictionary;
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object fvOptions;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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disk
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{
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type rotorDisk;
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selectionMode cellZone;
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cellZone rotatingZone;
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fields (U); // Names of fields on which to apply source
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nBlades 3; // Number of blades
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tipEffect 0.96; // Normalised radius above which lift = 0
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inletFlowType local; // Inlet flow type specification
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inletVelocity (0 1 0);
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geometryMode specified;
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origin (0 0 0);
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axis (0 1 0);
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refDirection (0 0 1); // Reference direction
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// - used as reference for psi angle
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rpm 1000;
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//pointAbove (0 0 0.25);
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trimModel fixedTrim; // fixed || targetForce
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rhoRef 1000;
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rhoInf 1;
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fixedTrimCoeffs
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{
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theta0 0;
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theta1c 0;
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theta1s 0;
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}
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flapCoeffs
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{
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beta0 0; // Coning angle [deg]
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beta1c 0; // Lateral flapping coeff (cos coeff)
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beta2s 0; // Longitudinal flapping coeff (sin coeff)
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}
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blade
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{
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data
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(
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(profile1 (0.1 -6 0.02))
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(profile1 (0.25 -6 0.02))
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);
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}
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profiles
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{
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profile1
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{
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type lookup;
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data
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(
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(-90 0.21 1.45)
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(-18 0.21 1.45)
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(-16 0.165 1.3)
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(-14 0.125 1.1)
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(-12 0.092 0.95)
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(-10 0.07 0.8)
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(-8 0.05 0.64)
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(-6 0.04 0.5)
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(-4 0.028 0.32)
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(-2 0.022 0.18)
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(0 0.02 0)
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(2 0.022 0.18)
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(4 0.028 0.32)
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(6 0.04 0.5)
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(8 0.05 0.64)
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(10 0.07 0.8)
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(12 0.092 0.95)
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(14 0.125 1.1)
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(16 0.165 1.3)
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(18 0.21 1.45)
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(90 0.21 1.45)
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);
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}
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}
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}
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// ************************************************************************* //
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@ -16,51 +16,31 @@ FoamFile
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ddtSchemes
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{
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default steadyState;
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}
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gradSchemes
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{
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default Gauss linear;
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limited cellLimited Gauss linear 1;
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grad(U) $limited;
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grad(k) $limited;
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grad(omega) $limited;
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}
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divSchemes
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{
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default none;
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div(phi,U) bounded Gauss linearUpwind unlimited;
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turbulence bounded Gauss linearUpwind limited;
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div(phi,k) $turbulence;
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div(phi,omega) $turbulence;
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div(phi,epsilon) $turbulence;
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div((nuEff*dev(T(grad(U))))) Gauss linear;
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div((nuEff*dev2(T(grad(U))))) Gauss linear;
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}
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laplacianSchemes
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{
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default Gauss linear corrected;
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}
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interpolationSchemes
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{
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default linear;
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}
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snGradSchemes
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{
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default corrected;
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}
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wallDist
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{
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method meshWave;
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}
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// ************************************************************************* //
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@ -16,43 +16,7 @@ FoamFile
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solvers
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{
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p
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{
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solver GAMG;
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smoother GaussSeidel;
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tolerance 1e-6;
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relTol 0.1;
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}
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"(U|k|omega|epsilon)"
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{
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solver smoothSolver;
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smoother symGaussSeidel;
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tolerance 1e-6;
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relTol 0.1;
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}
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}
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SIMPLE
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{
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nNonOrthogonalCorrectors 0;
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consistent yes;
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residualControl
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{
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U 1e-4;
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p 1e-3;
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"(k|epsilon|omega)" 1e-3;
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}
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}
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relaxationFactors
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{
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equations
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{
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U 0.95;
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"(k|omega|epsilon)" 0.95;
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}
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}
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// ************************************************************************* //
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@ -19,4 +19,5 @@ FoamFile
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//- minFaceWeight (0 -> 0.5)
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//minFaceWeight 0.02;
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// ************************************************************************* //
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@ -163,4 +163,5 @@ meshQualityControls
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mergeTolerance 1e-6;
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// ************************************************************************* //
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@ -24,4 +24,5 @@ rotatingZone.obj
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#includeEtc "caseDicts/surface/surfaceFeatureExtractDict.cfg"
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}
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// ************************************************************************* //
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